Seal carrier attachment for a turbomachine

Abstract

A housing structure for a turbomachine having a stationary blade ring annularly surrounding a flow channel, and having a seal carrier ring which also annularly surrounds the flow channel, the stationary blade ring and the seal carrier ring being connected to each other, and either the stationary blade ring or the seal carrier ring having a one-sidedly open receptacle in the radial direction in relation to the flow channel and a radially projecting engagement area which corresponds to the connected seal carrier ring or stationary blade ring and which is held in a form-fitting manner in the axial direction and in the radial direction in the direction of the closed side of the receptacle but is freely movable with respect to the connected receptacle and the seal carrier ring or stationary blade ring having this receptacle in the radially opposite direction in the direction of the receptacle opening.

Description

[0001]This claims the benefit of European Patent Application No. EP 12190529.3, filed Oct. 30, 2012 and hereby incorporated by reference herein.[0002]The present invention relates to a housing structure for a turbomachine, in particular for a gas turbine or an aircraft engine.BACKGROUND[0003]In turbomachines such as stationary gas turbines or aircraft engines, air is taken in along a flow channel, compressed and combusted together with fuel in a combustion chamber, the combustion gases being subsequently expelled via the flow channel for the purpose of driving rotors in a turbine.[0004]The flow channel is circumferentially surrounded by a housing structure, the rotors or moving blades provided on the rotors being required to abut the housing structure as tightly as possible to avoid flow losses. To achieve this, so-called rub coatings or run-in coatings are provided on the inside of the housing in the area of the rotating moving blades and are in rubbing contact with sealing tips si...

AI Technical Summary

Benefits of technology

The present invention provides a housing structure for a turbomachine which allows for the efficient and easy placement of a seal carrier ring. This design allows for significant flexibility in the placement of adjacent components. The seal carrier ring is connected to a stationary blade ring in a way that allows for a receptacle to hold the components securely in place. The connection occurs at the vane platform, which allows for a more flexible design and easy assembly. The invention also provides a sealing effect that improves the sealing of the flow channel. This connection can be used in cases where there is thermal expansion.

Problems solved by technology

However, the problem exists that this approach may make the assembly of the seal carrier segments or the seal carrier ring complex, and the freedom of designing the housing structure or executing the stationary blade suspension may be limited, with the result that aerodynamically unfavorable conditions may set in.

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